WO2010125172A3 - Device for spatially orienting at least two subgroup components and method - Google Patents

Device for spatially orienting at least two subgroup components and method Download PDF

Info

Publication number
WO2010125172A3
WO2010125172A3 PCT/EP2010/055878 EP2010055878W WO2010125172A3 WO 2010125172 A3 WO2010125172 A3 WO 2010125172A3 EP 2010055878 W EP2010055878 W EP 2010055878W WO 2010125172 A3 WO2010125172 A3 WO 2010125172A3
Authority
WO
WIPO (PCT)
Prior art keywords
subgroup
subgroup components
components
shell
positioning apparatuses
Prior art date
Application number
PCT/EP2010/055878
Other languages
German (de)
French (fr)
Other versions
WO2010125172A2 (en
Inventor
Ulrich Stark
Jörg SCHRICKEL
Wolfgang Brandt
Original Assignee
Airbus Operations Gmbh
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Priority to BRPI1009916A priority Critical patent/BRPI1009916A2/en
Priority to CN201080029745.0A priority patent/CN102802867B/en
Priority to RU2011148902/02A priority patent/RU2533984C2/en
Priority to EP10719318.7A priority patent/EP2424780B1/en
Priority to JP2012507776A priority patent/JP2012525266A/en
Priority to CA2760720A priority patent/CA2760720A1/en
Priority to US13/318,364 priority patent/US9132924B2/en
Publication of WO2010125172A2 publication Critical patent/WO2010125172A2/en
Publication of WO2010125172A3 publication Critical patent/WO2010125172A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • B23P19/10—Aligning parts to be fitted together
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/01—Aircraft parts

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automatic Assembly (AREA)
  • Control Of Position Or Direction (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)

Abstract

The invention relates to a device for spatially orienting at least two large-size subgroup components, in particular at least one side shell (7,8), at least one upper shell (12), at least one lower shell (11), and/or at least one floor framework, in relation to each other to integrate a component, in particular a fuselage section of an aircraft, comprising: a) at least two positioning apparatuses for accommodating one subgroup component each, in particular at least two side shell positioners (2,3), at least one upper shell positioner (5), and/or at least one lower shell positioner (4), b) at least one measuring apparatus for detecting a plurality of measurement data, in particular position data of the subgroup components and/or of the positioning apparatuses, c) at least one control and/or regulating apparatus (19), in particular at least one CNC controller, and d) at least one neural network (20). The neural network (20) integrated according to the invention into the device allows the subgroup components to be brought into a specified target geometry by means of simultaneous movement of the positioning apparatuses in the shortest amount of time and with high accuracy. The control and/or regulating apparatus (19) is used preferably to subsequently orient the subgroup components in relation to each other by means of simultaneously executed linear movements of the positioners. The invention further relates to a method for orienting subgroup components.
PCT/EP2010/055878 2009-05-01 2010-04-30 Device for spatially orienting at least two subgroup components and method WO2010125172A2 (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
BRPI1009916A BRPI1009916A2 (en) 2009-05-01 2010-04-30 device for specially aligning at least two subset components and method to the same.
CN201080029745.0A CN102802867B (en) 2009-05-01 2010-04-30 For the apparatus and method of spatially directed at least two subassemblys
RU2011148902/02A RU2533984C2 (en) 2009-05-01 2010-04-30 Device and method for spatial orientation of at least two components of subgroups
EP10719318.7A EP2424780B1 (en) 2009-05-01 2010-04-30 Device for spatially orienting at least two subgroup components and method
JP2012507776A JP2012525266A (en) 2009-05-01 2010-04-30 Apparatus and method for three-dimensionally aligning at least two subassemblies with each other
CA2760720A CA2760720A1 (en) 2009-05-01 2010-04-30 Device for spatially aligning at least two subassembly components and method for this
US13/318,364 US9132924B2 (en) 2009-05-01 2010-04-30 Device for spatially orienting at least two subgroup components and method

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US17450209P 2009-05-01 2009-05-01
DE102009018991.2 2009-05-01
US61/174,502 2009-05-01
DE102009018991A DE102009018991A1 (en) 2009-05-01 2009-05-01 Device for the spatial alignment of at least two subassembly components and method

Publications (2)

Publication Number Publication Date
WO2010125172A2 WO2010125172A2 (en) 2010-11-04
WO2010125172A3 true WO2010125172A3 (en) 2011-05-26

Family

ID=42813636

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2010/055878 WO2010125172A2 (en) 2009-05-01 2010-04-30 Device for spatially orienting at least two subgroup components and method

Country Status (9)

Country Link
US (1) US9132924B2 (en)
EP (1) EP2424780B1 (en)
JP (1) JP2012525266A (en)
CN (1) CN102802867B (en)
BR (1) BRPI1009916A2 (en)
CA (1) CA2760720A1 (en)
DE (1) DE102009018991A1 (en)
RU (1) RU2533984C2 (en)
WO (1) WO2010125172A2 (en)

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CN105035346B (en) * 2014-04-30 2018-10-23 波音公司 Modularization struts
CN106458336B (en) * 2014-06-27 2020-08-21 C系列飞机有限合伙公司 Reshaping of deformed parts for assembly
US10406593B2 (en) 2014-07-09 2019-09-10 The Boeing Company Method of using a tower for accessing an interior of a fuselage assembly
US11131982B2 (en) 2014-09-17 2021-09-28 The Boeing Company Fuselage manufacturing system
US9682788B2 (en) 2014-09-17 2017-06-20 The Boeing Company Fuselage manufacturing system
US9927227B2 (en) 2014-09-17 2018-03-27 The Boeing Company Metrology system for generating measurements of fuselage sections
US9453720B2 (en) 2014-09-17 2016-09-27 The Boeing Company Metrology system for generating measurements of fuselage sections
US11273930B2 (en) 2014-09-17 2022-03-15 The Boeing Company Cradle system for shaping fuselage sections
DE102014116560A1 (en) 2014-11-12 2016-05-12 Airbus Operations Gmbh A method and apparatus for securing an aircraft or spacecraft component to a fuselage section of an aircraft or spacecraft
US9737967B2 (en) * 2014-12-17 2017-08-22 Embraer S.A. Universal magnetic table jig assemblies and methods for positioning a workpiece, especially for the fabrication of aircraft structural components
GB201505400D0 (en) 2015-03-30 2015-05-13 Rolls Royce Plc Multi coordinate reference system for positioning bladed drum
US10162339B2 (en) * 2015-04-08 2018-12-25 Sciperio, Inc Automated manufacturing using modular structures and real time feedback for high precision control
CN106563932A (en) * 2015-10-08 2017-04-19 陕西飞机工业（集团）有限公司 Novel butt joint jig
GB201522174D0 (en) * 2015-12-16 2016-01-27 Univ Nottingham Orientation and/or position monitoring and control
ES2929413T3 (en) * 2016-05-27 2022-11-29 Airbus Operations Gmbh Production system for the automated assembly of vehicle components and method for controlling a production system
CN108459557B (en) * 2017-07-26 2021-11-19 华中科技大学 Part machining size evaluation method
EP3511252B1 (en) * 2018-01-11 2020-12-16 Airbus Operations GmbH Production system for the automated assembly of vehicle components and method for controlling a production system
FR3090586A1 (en) * 2018-12-20 2020-06-26 Airbus Operations System and method for determining the spacing between two rooms using eddy current sensors
DE102020204993A1 (en) * 2020-04-21 2021-10-21 Premium Aerotec Gmbh Assistance system and method for positioning a first component relative to a second component and remote control for an assistance system
EP4177171A1 (en) * 2021-11-03 2023-05-10 The Boeing Company Method and system for transporting a workpiece in a manufacturing environment
NL2029840B1 (en) * 2021-11-19 2023-06-13 Boeing Co Systems and methods for supporting a workpiece in a manufacturing environment
EP4177170A1 (en) 2021-11-03 2023-05-10 The Boeing Company Systems and methods for supporting a workpiece in a manufacturing environment
NL2029839B1 (en) * 2021-11-19 2023-06-13 Boeing Co Method and system for transporting a workpiece in a manufacturing environment

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Also Published As

Publication number Publication date
CN102802867B (en) 2015-08-26
BRPI1009916A2 (en) 2016-03-15
CN102802867A (en) 2012-11-28
US20120130528A1 (en) 2012-05-24
RU2011148902A (en) 2013-06-10
RU2533984C2 (en) 2014-11-27
JP2012525266A (en) 2012-10-22
EP2424780A2 (en) 2012-03-07
DE102009018991A1 (en) 2010-11-04
CA2760720A1 (en) 2010-11-04
WO2010125172A2 (en) 2010-11-04
US9132924B2 (en) 2015-09-15
EP2424780B1 (en) 2016-03-30

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